By N.A.V. Piercy

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**Sample text**

Nevertheless, a design for the short arm can be arrived at by experiment, such that the gauge shows no pressure difference when the tube is given any Adding to the whole system of tube and air velocity, large or small. a velocity equal and opposite to that of the tube converts the case of motion to that of a stationary tube immersed in an initially uniform The pressure communicated is then the same when the air-stream. tube is immersed in uniform flow or in stationary air. Thus the tube To cope correctly transmits the static pressure of a uniform motion.

Nevertheless, a design for the short arm can be arrived at by experiment, such that the gauge shows no pressure difference when the tube is given any Adding to the whole system of tube and air velocity, large or small. a velocity equal and opposite to that of the tube converts the case of motion to that of a stationary tube immersed in an initially uniform The pressure communicated is then the same when the air-stream. tube is immersed in uniform flow or in stationary air. Thus the tube To cope correctly transmits the static pressure of a uniform motion.

P 1 . D. 2 pt : . A sin 2 a = 0, = 0. (34) of equation This now in the AERODYNAMICS 34 [CH. This equation is independent of a. Hence the arithmetic mean of the normal components of pressure on any pair of perpendicular faces through G is the same. 27. The Static Pressure in Let us write a Flow : -#=*(#! + PI = *(# + Pyy) ( 36) has been found possible to say, x and y are any directions at Then p does not depend upon direction right angles to one another. and is the compressive pressure we shall have in mind when referring to the static pressure/ or simply the pressure, at a point of a fluid in motion.